Design to absorb or dissipate the impact energy during landing Typically use springs, oleo strut(hydraulic shock)

* Most common type of non shock absorbing landing gear * Utilize flexible spring steel, aluminum, or composite strut

While not a primary nose wheel steering system, (blank blank) plays a role in steering on the ground. By applying more brake pressure to one main landing gear wheel than the other, the aircraft can pivot, assisting in making turns, especially in situations where nose wheel steering alone may be insufficient.

utilizes bungee cord or rubber cords as form of shock absortion during landing process

Landing gear contributes to the stability of the aircraft during takeoff, landing, and taxiing

is a type of steering mechanism in aircraft where the direction of the nose wheel is controlled by the pilot's input on the rudder pedals in the cockpit. This system is commonly

is commonly used for nose wheel steering.

* Do not have the capacity to absorb or dissipate landing impact * Often found in smaller, lightweight aircraft or those designed for operation or very smooth surface

It provides better ground visibility for pilots, improved handling during takeoff and landing, and greater stability on the ground. 1 Wheel in front 2 Wheel in Back

During the landing phase, the aircraft experiences a considerable amount of vertical force and impact as it touches down on the runway.

3 Primary Function of Landing Gear

It’s crucial components responsible for supporting an aircraft during landing, takeoff and while on ground designed for stability

typically flat or slightly curved structures made of sturdy materials like metal, composite materials, or even reinforced plastics

* Shock load transfer to the airframe is direct with this * Curved spring steel landing struts

of an aircraft is a crucial component that plays a significant role in ground maneuverability. This system allows the pilot to control the direction of the aircraft during taxiing, takeoff, and landing on the ground.

Some aircraft feature a combination of tiller and pedal controls. This allows pilots to choose the method that best suits the specific taxiing situation. The tiller might be used for sharp turns or precise maneuvering, while pedals can be used for more general steering.

offer simplicity, lower maintenance costs, and better visibility during flight. However, they can be more challenging to handle on the ground due to limited forward visibility. 2 Wheel in front 1 Wheel in back

allows an aircraft to operate both on land and on water. versatile and can be used for operations in various environments, such as flying to remote locations with limited landing options.

Self contained hydraulic units that support an aircraft while on the ground and protect the structure during landing

The landing gear provides the necessary support to hold the aircraft's weight during various phases of flight, especially during landings and ground operations

can be stowed inside the aircraft's fuselage during flight, reducing drag and improving aerodynamic efficiency. 1 Wheel in front 2 Wheel in back